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Future Space-Transport-System Components under High Thermal and Mechanical Loads: Results from the DFG Collaborative Research Center TRR40 1st ed. 2021 [Mīkstie vāki]

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  • Formāts: Paperback / softback, 419 pages, height x width: 235x155 mm, weight: 658 g, 213 Illustrations, color; 60 Illustrations, black and white; IX, 419 p. 273 illus., 213 illus. in color., 1 Paperback / softback
  • Sērija : Notes on Numerical Fluid Mechanics and Multidisciplinary Design 146
  • Izdošanas datums: 27-Oct-2021
  • Izdevniecība: Springer Nature Switzerland AG
  • ISBN-10: 3030538494
  • ISBN-13: 9783030538491
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  • Mīkstie vāki
  • Cena: 91,53 €*
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Future Space-Transport-System Components under High Thermal and Mechanical Loads: Results from the DFG Collaborative Research Center TRR40 1st ed. 2021Palielināt
  • Formāts: Paperback / softback, 419 pages, height x width: 235x155 mm, weight: 658 g, 213 Illustrations, color; 60 Illustrations, black and white; IX, 419 p. 273 illus., 213 illus. in color., 1 Paperback / softback
  • Sērija : Notes on Numerical Fluid Mechanics and Multidisciplinary Design 146
  • Izdošanas datums: 27-Oct-2021
  • Izdevniecība: Springer Nature Switzerland AG
  • ISBN-10: 3030538494
  • ISBN-13: 9783030538491
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9783030538491.html
This open access book presents the findings of Collaborative Research Center Transregio 40 (TRR40), initiated in July 2008 and funded by the German Research Foundation (DFG). Gathering innovative design concepts for thrust chambers and nozzles, as well as cutting-edge methods of aft-body flow control and propulsion-component cooling, it brings together fundamental research undertaken at universities, testing carried out at the German Aerospace Center (DLR) and industrial developments from the ArianeGroup.  With a particular focus on heat transfer analyses and novel cooling concepts for thermally highly loaded structures, the book highlights the aft-body flow of the space transportation system and its interaction with the nozzle flow, which are especially critical during the early phase of atmospheric ascent. Moreover, it describes virtual demonstrators for combustion chambers and nozzles, and discusses their industrial applicability. As such, it is a timely resource for researchers, graduate students and practitioners.





 





 
Collaborative Research for Future Space Transportation Systems.-
Innovative Cooling for Rocket Combustion Chambers.- Film Cooling in Rocket
Nozzle.- Heat Transfer in Pulsating Flow and its Impact on Temperature
Distribution and Damping Performance of Acoustic Resonators.- Eects of a
Launchers External Fow on a Dual-Bell Nozzle Flow.- Interaction of Wake and
Propulsive Jet Flow of a Generic Space Launcher.- Numerical Analysis of the
Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.